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Aircraft program

Beyond Aero One

In production
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6–8 passenger hydrogen-electric business aircraft designed for an 800 nautical mile mission at 300 KTAS, with a maximum speed of 360 KTAS. The aircraft is powered entirely by hydrogen fuel cells, with a battery-free 2.4 MW electrical architecture and twin aft-mounted electric propfans. Six Type IV tanks store 193 kg of gaseous hydrogen at 700 bar. The aircraft is being developed for EASA CS-25 / FAA Part 25 certification, with certification targeted for the early 2030s.

Lift type
Fixed wing
Assembly
Factory-built
Control
Piloted
Engine type
Electric
Application
Passenger small

Design & construction

The aircraft as engineered: what it is built from, the systems it flies with, and its configuration — each box a theme.

Airframe & structure
Primary structure
Composite
Wing
Composite
Landing gear
Retractable tricycle
Pressurisation
Unpressurised
Configuration & certification
Wing position
Low
Tail
Conventional
continued
Certification
Part 25
Minimum crew
1

Notable technologies — each tag names a technology on our research record for this aircraft, with its fitting status: Primary, Standard, Option or Planned.

Hydrogen fuel-cell propulsion Planned

Technical reference compiled with AI research; a value appears only where two independent research passes and a web fact-check agree. Gaps are deliberate.

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Type variants

VariantLaunch / first flightProduction endNotes
Beyond Aero One2023 / Hydrogen-electric business aircraft, designed from the outset for hydrogen propulsion. Also designated BYA-I.

Airframer

Beyond AeroNews

The program’s dated history — milestones, contracts, supplier selections and facilities, each linked to its source. Log in to view.

Information on this page is compiled from a variety of published sources; links do not necessarily imply recommendation or confirmation by the airframe manufacturer.

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